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Final rule 2025-12873

Airworthiness Directives; Airbus Helicopters

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS-365N2, AS 365 N3, EC 155B, EC155B1, SA- 365N, and SA-365N1 helicopters. This AD was prompted by reports of loss of tightening torque between the upper ball bearing end and the main rotor (MR) servo-control. This AD requires inspecting the tightening torque and, depending on the results, taking corrective action. This AD also requires reporting information. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-07-31 22:49:02 UTC.

Source-supplied record

Document details

Document number
2025-12873
Published
Jul 10, 2025
Effective
Aug 14, 2025
Comments close
Not supplied
Federal Register citation
90 FR 30581

Docket identifiers

  • Docket No. FAA-2025-0617
  • Project Identifier MCAI-2024-00331-R
  • Amendment 39-23075
  • AD 2025-13-09

CFR references

  • Title 14, part 39